GB2375354A

GB2375354A - Method of heating iron alloys

Info

Publication number: GB2375354A
Application number: GB0219615A
Authority: GB
Inventors: Masayuki Tsuchiya; Hiroaki Ueno
Original assignee: Honda Motor Co Ltd
Current assignee: Honda Motor Co Ltd
Priority date: 1998-07-14
Filing date: 1999-07-14
Publication date: 2002-11-13
Anticipated expiration: 2019-07-14
Also published as: DE19981496B3; GB2345699A; WO2000004198A1; GB0009121D0; US6616777B1; US20040105776A1; GB0219615D0; GB2345699B; GB2375354B

Abstract

An iron-based alloy which comprises a chilled structure (i.e. comprising ledburite) is heated into a semi-molten state wherein the average heating rate to the A<SB>1</SB> point on the alloys Fe-C equilibrium phase diagram is in the range of 0.5-6.0 {C/sec and the maximum temperature gradient in the alloy is 7 {C/mm. According to claim 1 a thixocast alloy is heated using this process. According to the examples the alloy is thixocast after heating using this process. Also disclosed are the following thixocast cast irons comprising 10-50 % by weight of eutectic crystals: I 1.8-2.5 wt. % C, 1.0-3.0 wt. % Si, 0.1-1.5 wt. % Mn, 0.5-3.0 wt. % Ni with the balance being Fe and impurities; II 1.8-2.5 wt. % C, 1.0-3.0 wt. % Si, 0.8-1.5 wt. % Mn with the balance being Fe and impurities; III 1.8-2.5 wt. % C, 1.0-3.0 wt. % Si, 0.6-1.5 wt. % Mn, at least one of 0.2-3.0 wt. % Ni and 0.05-0.6 wt. % Ti with the balance being Fe and impurities (Mn+Ni+Ti / 0.8 wt. %).

Description

* 1 2375354

THIXOCAST Fe-BASED ALLOY MATERIAL AND PROCESS FOR HEATING THE SAME

FIELD OF THE INVENTION

The present invention relates to a thixocast Fe-based 5 alloy material, and a process for heating the same.

BACKGROUND ART

In carrying out a thixocasting process, a procedure is employed which comprises heating an Fe-based alloy material into a semi-molter statein which asolldphase(asubstantially 10 solid phase and this term will also be applied hereinafter) and a liquid phase coexist, pouring the semi- molten Fe-based alloy material under a pressure into a cavity in a casting mold, and solidifying the semi-molten Fe-based alloy material under a pressure. 15 There is such a known Fe-based alloy material having a eutectic crystal amount Ec set in a range of 50 % by weight s Ec 70 % by weight (see Japanese Patent Application Laid-open No.5-43978). However, if the eutectic crystal amount Ec is set to be 20 equal to or larger than 50 % by weight, the amount of graphite precipitated is increased in such an Fe-based alloy material, and hence, the mechanical properties of a cast product are substantially equivalent to those of a cast product made by casting. Therefore, with the conventional material, it is 25 impossible to achieve an intrinsic purpose of enhancing the

mechanical properties of the cast product made by the thixocasting process.

In a quenched area such as a thinner portion in the cast structure of the cast product, a portion which has been a 5 spherical solid phase is transformed into a mixed structure of austenite end martensite. On the other hand, in a slowly cooled area such as a thicker portion, a portion which has been a sphericalsolidphaseistransformedinto apearlite structure.

Portions which have been liquid phases in both the areas are 10 transformed into aledeburite structure (a chilled structure) If such a cast productis subjected to athermaltreatment, the following problem also arises: Graphite is finely precipitated in the quenched area, while it is precipitated in a coalesced manner in the slowly cooled area. As a result, the 15 mechanicalproperties of both the areas are different from each other. For this reason, it is impossible to produce a cast product having mechanical properties uniform over the whole thereof. Further, in the thixocasting process, the temperature of 20 the semi-molten Fe-based alloy material, namely, the casting temperature is low as compared with the temperature of a molten metal. Therefore, when a cast product having a smaller thickness or haying a complicated shape is produced by casting, the semi-molten Fe-based alloy material is cooled rapidly by 26 the casting mold, and as a result, a portion which has been a liquid phase has a chilled structure having a low toughness.

The chilled structure is liable to become a starting point for cracking on the solidification and shrinkage of the material, which is undesirable. Therefore, a measure to form an inner wall of a casting mold from a carbon material such as graphite 5 is employed to moderate the quenching of the materiel. However, the following problem is encountered by utilizing the thixocasting process: The carbon material is worn violently and for this reason,,the replacement of the casting mold must be performed frequently, which is uneconomic, and moreover, 10 which results in a reduced productivity.

On the other hand, if the stability and productivity of components and me/allographic structure and the like of the Fe-based alloy material are taken into consideration, it is optimalto produce such materialbya continuous casting process.

15 In the continuous casting process, however, the cooling rate of the Febased alloy material is high, and for this reason, a chilled structure may beproducedin the materialin some eases.

When such an Fe-based alloy material is heated, the following problem arises: The temperature gradient of the inside of the 20 material is increased depending on heating conditions, whereby cracks are produced in the material, and the material cannot be heated to a target temperature during induction-heating.

DISCLOSURE OF THE INVENTION

Accordingly, it is an object of the present invention to 25 provide a thixocast Fe-based alloy material of the above-

described type, from which a cast product having mechanical

properties which are more excellent then those of a east product made by casting, and which are uniform over the whole of the cast product, can be produced.

To achieve the above object, according to the present 5 invention, there is provided a thixocast Fe-based alloy material comprising 1.8 by weight s C s 2.5 by weight, 1.0 by weight Si 3.0 by weight, 0.1 by weight Mn 1.5 % by weight, 10 0.5 % by weight s Ni 3.0 by weight, and as the balance, iron (Fe) including inevitable impurities, and wherein a eutectic crystal amount Ec is in a range of 10 by weight < Ec < 50 by weight.

A semi-molten Fe-based alloy material having liquid and 15 solid phases coexisting therein is prepared by subjecting the Fe-based alloy material having the above composition to a heating treatment. In this semi-molten Fe-based alloy material, the liquid phase produced by a eutectic melting has a large latent heat. As a result, in the course of 20 solidification of the semi-molter Fe-based alloy material, the liquid phase issuppliedina sufficient amount around the solid phase in response to the solidification and shrinkage of the solid phase, andis then solidified. Therefore,the generation of voids of a micron order in the cast product is prevented.

25 In addition, the amount of graphite precipitated can be reduced

by setting the eutecticcrystalamountEc in the above-described range. Thus, it is possible to enhance the mechanical properties, i.e., the tensile strength, the Young's modulus, the fatigue strength and the like of the cast product. In the 5 Fe-based alloy material with the eutectic crystal amount Ec in the above-described range, it is possible to lower the casting temperature of the Fe-based alloy material, thereby providing the prolongation of,the life of a casting mold.

However, if the eutectic crystal amount Ec is equal to 10 or smaller than 10 % by weight, the casting temperature of the Fe-based alloy material approximates to a liquidus temperature due to the small eutectic crystal amount Ec. Therefore, a heat load of a materialtransporting equipment to a pressure casting apparatus is high, thereby making it impossible to carry out 15 the thixocasting. Ontheotherhand,adisadvantageraisedwhen Ec 50 by weight is as described above.

In the above-described composition, manganese (Mn) is a cementite and austenite producing element, and nickel (Ni) is an austenite producing element. Therefore, Mn and Ni inhibit 20 the slowly cooled area from being transformed into a pearlite structure. Thus,thecast structure of the entire cast product is such that a portion which has been a solid phaseis transformed into a mixed structure of austenite and martensite, and a portion which has been a liquid phase is transformed into a 25 ledeburite structure.

By subjecting such a cast product into a predetermined thermal treatment, a cast product having a uniformly thermally treated structure with fine graphite dispersed in a mixed structure of ferrite and pearlite is produced. This cast 5 product has mechanical properties uniform over the whole thereof. In the above-described composition, carbon (C) and silicon (Si) participate in the eutectic crystal amount, and the C content and the Si content are set in the above-described 10 ranges to control the eutectic crystal amount in the above-

describedrange. However,iftheCcontentissmallerthanl.8% by weight, the casting temperature must be high, even if the Sicontentisincreased toincrease the cutecticcrystalamount.

Therefore, the advantage of the thixocasting is degraded. On 15 the other hand, if C > 2.5 by weight, the amount of graphite is increased. For this reason, the mechanical properties of the cast product is degraded, and the eutectic crystal amount is increased and hence, the handlability of the semi-molten Fe-based alloy material is deteriorated. If the Si content is 20 smaller than 1.0 by weighs, the casting temperature is raised as the case where the C content is smaller than 1.8 by weight.

On the other hand, if Si > 3.0 by weight, silico-ferrite is produced and for this reason, the mechanical properties of the cast product cannot be enhanced.

25 Manganese (Mn) functions as a deoxidizing agent and is required for producing cementite. However, if the Mn content

is smaller than 0.1 by weight, the deoxidizing effect is smeller end for this reason,defects due toinclusionof en oxide caused by the oxidation of the molten metal and due to bubbles are liable to be produced. On the other hand, if Mn > 1.5 5 by weight, the amount of cementite [(FeMn)3C] crystallized is increased. For this reason, it is difficult to finely divide the large amount of cementite by a thermal treatment, resulting in a reduced toughness and a reduced cutting property of a cast product. 10 Nickel (Ni) is an austenite producing element, as described above, and has an effect which allows austenite to exist in a very small amount at normal temperature to enclose impurities in the austenite, thereby enhancing the toughness.

To provide such effect, it is necessary to set the Ni content 15 at about 1 by weight. However, if the Ni content is smaller than 0.5 by weight, the addition of nickel is meaningless.

Ontheotherhand,ifNi>3.0%byweight,amatrixistransformed i into a martensite structure with an increased hardness in the course of cooling following a cementite-eliminating thermal 20 treatment.

It is another object of the present invention to provide athixocast Febased alloy materialof the above-described type, wherein the generation of cracks in a thin cast product and the like can be avoided.

25 To achieve the above object, according to the present invention, there is provided a thixocast Fe-based alloy

material comprising 1.8 % by weight C s 2.5 by weight 1.0 % by weight s Si s 3.0 % by weight 0.8 by weight s Mn s 1.5 % by weight, and 5 as the balance, iron (Fe) including inevitable impurities, and wherein a eutectic crystal amount Ec being in a range of /, 10 % by weight < Ec 50 % by weight.

When a thixocasting is carried out using the Fe-based 10 alloy material having the above composition and using a conventional casting mold, a portion which has been a solid phase is transformed into a mixed structure of austenite and martensite in the entire thin cast product due to the presence of Mn which is an austenite producing element, and a portion 15 which has been a liquid phase is transformed into a ledeburite structure. In this way, the toughness of the entire structure is enhanced by the austenite remaining in the portion which has been the solid phase. Therefore, in the thin cast product and the like, the generation of cracks due to the solidification 20 and shrinkage is avoided. In addition, it has been made clear that if the above Fe-based alloy material is used, the pearlite transformation of a thick portion cooled at a low speed in the cast product can be inhibited to ensure that austenite remains in the portion which has been the solid phase.

25 In the alloy composition of this material, manganese (Mn)

is an austenite producing element and has an effect of permitting austenite to remain in the portion which has been the solid phase, as described above. If the Mn content is smaller than 0.8 % by weight, the amount of austenite remaining 5 in the portion which has been the solid phase is insufficient, and the amount of austenite crystallized in ledeburite presenting a chilled structure is also insufficient. On the other hand, if Mn > 1.5 % by weight, the amount of cementite [(FeMn)3C] precipitated in ledeburite is increased, resulting 10 in reduced toughness end cutting properly of a product. Mn also has a function as a deoxidizing agent.

The reason why the eutectic crystal amount Ec, the C content and the Si content are limited in the Fe-based alloy material is the same as described above.

15 In addition, according to the present invention, there is provided a thixocast Fe-based alloy material, comprising carbon (C) of a content in a range of 1.8 % by weight s C s 2.5 % by weight, silicon (Si) of a content in a range of 1.0 % by weight s Si s 3.0 % by weight, manganese (Mn) of a content in a range 20 of 0.6 % by weight s Mn s 1.5 % by weight, at least one of nickel (Ni) of a content in a range of 0.2 % by weight s Ni s 3.0 % by weight and titanium (Ti) of a content in a range of 0.05 % by weight s Ti s O.6 % by weight, the total sum of the Mn content, the Ni content and the Ti content being equal to or larger than 25 0.8 % by weight (Mn + Ni + Ti 0.8 by weight), and the balance

of iron (Fe) including inevitable impurities, a eutectic crystal amount Ec being in a range of 10 % by weight < Ec < 50 by weight.

If the Fe-based alloy material having the above 5 composition is used, the generation of cracks due to the solidification and shrinkage can be further reliably avoided in a thin cast product.

The reason why the eutectic crystal amount, the C content and the Si content are limited in the Fe-based alloy material 10 is the same as described above.

Nickel (Ni), which is an austenite producing element, acts to further promote the remaining of austenite and to encloseimpuritiesin the remaining austenite for harmlessness.

Namely, nickel (Ni) has an effect of dispersing the impurities 15 reducing the toughness into the austenite rich in toughness, thereby preventing the impurities from influencing the mechanical properties. In addition, nickel (Ni) also has an effect of preventing the pearlite transformation of a portion cooled slowly such as a thick portion. However, If the Ni 20 content is smaller than 0.2 % by weight, the addition of nickel is meaningless. On the other hand, if the Ni content is larger than 3.0 % by weight, when the cast product is subjected to a thermaltreatmentin order to ensure that cementite disappears, thereby forming spherical fine graphite grains, the 25 precipitated graphite grains are agglomerated at points at points to bring about a reduction in toughness. In addition,

the matrixistransformedintomartensiteby the cooling carried out after the thermal treatment, resulting in an increased hardness. Further, the addition of an excessive amount of nickel brings about an increase in material cost.

5 Titanium(Ti)hasan effect of finely dividing the crystal grains in the solid phase to further enhance the toughness of the cast product. However, if the Ti content is smaller than 0.05 % by weight, the,addition of titanium is meaningless. On the other hand, if Ti > 0.6 % by weight, Tic is precipitated 10 and for this reason, the cutting property is reduced and the flowability of the molten metal is reduced, resulting in the generation of casting defects.

The lower limit value of the Mn content may be decreased down to 0.6 by weight, lower than that of the Fe-based alloy 15 material, because of the containment of titanium (Ti) and/or nickel (Ni). The reason why the upper limit value of the Mn content is limited is the same as described above.

i Even in a casting process by casting, it is possible to allow austenite to remain, but for this purpose, the cooling 20 rate must be managed extremely severely. According to the present invention, theremainingofausteniteinaportionwhich has been a solid phase has been realized in the thixocasting process by specifying the total amount of the Mn content and the Ni and Ti contents (or the Ni or Ti content). A lower limit 25 value of the total amount of the Mn content and the Ni and Ti contents(ortheNiorTicontent),0.8%byweight,isacondition

for providing the above-described effect without being influenced by the cooling rate.

It is desirable that the solid phase rate R in the semi-molter Fe-based alloymaterialin the thixocasting process 5 is larger then 50%. This makes it possible to shift the casting temperature to a lower level to prolong the life of a pressure casting apparatus. If the solid phase rate R is equal to or smaller than 50 %, the amount of the liquid phase is increased.

For this reason, when a short columnar semi-molten Fe-based 10 alloy material is transported in a standing state, the self-standing property thereof is degraded, and the handlability thereof is also degraded.

Further, it is an object of the present invention to provide a heating process, by which a thixocast Fe-based alloy 15 material having a chilled structure can be heated into a semi-molten state without generation otcracksin the material.

To achieve the above object, according to the present invention, there is provided a process for heating a thixocast Fe-based alloy material having a chilled structure into a 20 semi-molten state in which solid and liquid phases coexist, wherein the average rate HR Of heating to a point A1 in an Fe-C based equilibrium diagram is set in a range of 0.5 C/sec s HR s 6. 0 C/sec, and the maximum temperature gradient TG of the inside of the Febased alloy material per unit distance is set 25 at TG S 7 C/mm.

The average rate HR of heating to a point Aland the maximum temperature gradient TG are specified as described above, the cracking due to the heating of the Fe-based alloy material haying the chilled structure can beprevented,and the oxidation 5 of the material and the coalescence of crystal grains cannot occur. After the temperature exceeds the point Al, the heating rate is increased to effect the decomposition of dendrite and the spheroidization,of the solid phase. At this time, a y phase appears in the Fe-based alloy material, resulting in an 10 enhanced toughness of the material. Therefore, even if the heating rate is increased, cracks cannot be produced in the Fe-based alloy material.

Both of 6.0 C/sec which is an upper limit value for the average heating rate HR and 7 C/mm which is an upper limit value 15 for the maximum temperature gradient TG are limit values for preventing the generation of cracks due to the heating. If the average heating temperature HR islowerthanO.5 C/sec,problems of a reduction in producibility of a cast product, the coalescence of the solid phases and the oxidation of the 20 material surface arise.

The Fe-based alloy material which is the subject of the present invention is not limited to a material produced by a continuous casting process, and may be a material produced by casting and having a chilled structure.

25 To determine whether the Fe-based alloy material has a

chilled structure, it is a common practice to observe the material by a metal microscope, but it is convenient to use an ultrasonic velocity measuring process which is one of non-

destructive inspecting processes for a metal. The sonic 5 velocity Sv measured by the ultrasonic velocity measuring process is in a range of 5, 800 m/see Sv 6,000 m/see in a case of a steel. On the other hand, the reviews by the present inventors have made it clear that in a thixocast graphite-

crystallized Fe-based alloy material, a flake-formed graphite 10 phase is reflected as a defect to a measured value of sonic velocity and hence, the sonic velocity Sv assumes a low value in a range of 5,100 m/see s Sv s 5,450 m/see, but in an Fe based alloy material having a chilled structure, the sonic velocity assumes a value near that of a steel due to non 15 precipitation of graphite. Therefore, it can be determined from such a difference between the sonic velocities that if the sonic velocity Sv measured for the Fe-based alloy material by the ultrasonic velocity measuring process is a value 5,600 m/see, this material is an Fe-based alloy material having a 20 chilled structure.

BRIEF DESCRIPTION OF THE DRAWINGS

Fig.l is a sectional view of a pressure casting apparatus: Fig.2 is a graph showing the relationship between C and Si contents and a eutectic crystal amount Ec; 25 Fig.3 is a graph showing the relationship between a

heating temperature and a solid phase rate in correspondence to the C and Si contents; Fig.4 is a diagram for explaining a cast product; Fig.5A is a photomicrograph of the texture showing a cast 5 structure of a tip end portion A of example (1) of a cast product; Fig.5B is a photomicrograph of the texture showing a cast structure of an intermediate portion B of example (1) of the cast product;, Fig.5C is a photomicrograph of the texture showing a cast 10 structure of a base end portion C of example (1) of the cast product; Fig.6A is a photomicrograph of the texture showing a cast structure of a tip end portion A of example (la) of cast product; Fig.6B is a photomicrograph of the texture showing a cast 15 structure of an intermediate portion B of example (la) of the cast product; Fig.6C is a photomicrograph of the texture showing a cast structure of a base end portion C of example (la) of the cast product; 20 Fig.7A is a photomicrograph of the texture showing a first example of a thermally treated structure in the base end portion C of example (1) of the cast product; Fig.7B is a photomicrograph of the texture showing a first example of a thermally treated structure in the base end portion 25 C of example (la) of the cast product; Fig.8A is a photomicrograph of the texture showing a

second example of a thermally treated structure in the base end portion C of example (1) of the cast product; Fig.BB is a photomicrograph of the texture showing a second example of a thermally treated structure in the base end 5 portion C of example (la) of the cast product; Fig. 9Aisaphotomicrographof the texture showing a third example of a thermally treated structurein the tease end portion C of example (1) of,,the cast product; Fig.9Bisaphotomicrographof the texture showing a third 10 example of a thermally treated structurein the tease end portion C of example (la) of the cast product; Fig.10 is a sectional view of a pressure casting apparatus; Fig.11 is a plan view of an oil pump cover; 15 Fig.12 is a view of a first example of the oil pump cover; Fig.13 is a view of a second example of the oilpump cover; Fig.14 is a view of a third example of the oil pump cover; !," Fig.15 is a photomicrograph of the texture showing the first example of a me/allographic structure of the oil pump 20 cover; and Fig.16 is a photomicrograph of the texture showing the second example of a me/allographic structure of the oil pump cover; Fig.17 is an Fe-C based equilibrium diagram; 25 Fig.18 is a photomicrograph of the texture showing the me/allographic structure of an Fe-based alloy material having

a chilled structure; Fig.19 is a photomicrograph of the texture showing the me/allographic structure of an Fe-based alloy material having no chilled structure; 5 Fig.20 is asectionalviewof the Fe-based alloy materiel; Fig.21 is a graph showing the relationship between the heating time end the temperature of the Fe-based alloy materiel; Fig.22 is a graph showing the relationship between the average temperature of the Fe- based alloy material having the 10 chilled structure and the temperature difference; Fig.23 is a graph showing the relationship between the average heating rate and the maximum temperature gradient; Fig.24 is a graph showing the relationship between the average temperature of the Fe- based alloy material having no 15 chilled structure and the temperature difference; and Fig.25 is a graph showing the relationship between the ultrasonic velocity and the maximum temperature gradient.

BEST MODE FOR CARRYING OUT THE INVENTION

Embodiment I 20 pressure casting apparatus 1 shown in Fig.1 is used to produce a cast product by casting by using an Fe-based alloy material and utilizing a thixocasting process. The pressure casting apparatus 1 includes a stationary die 2 and a movable die 3 which have vertical mating surfaces 2a and 3a, 25 respectively,so that a east product forming cavity 4 is defined between both the mating surfaces 2a and 3a. A chamber 6 is

defined in the stationary die 2, so that a columnar semi-molten Fe-based alloy material 5 is placed horizontally in the chamber 6. The chamber 6 communicates with a base end of the cavity 4 through a truncated bore 7 and a gate 8. A sleeve 9 is 5 horizontally mounted to the stationery die2 to communicate with the chamber 6. A pressing plunger 10 is slidably received in the sleeve 9, so that it is inserted into and removed out of the chamber 6. The sleeve 9 has a material inlet 11 in an upper portion of a peripheral wall thereof. Each of the stationary 10 and movable dies 2 and 3 is formed of a Cu-Be based alloy as a copper-based alloy. The copper-based alloy which may be used is a Cu-Cr based alloy, Cu-Ni based alloy and the like. Pure copper may be utilized as a die forming material.

Fig.2 shows the relationship between the C end Si contents 15 and a eutectic crystal amount Ec in an Fe-based alloy material.

In Fig.2, a 10 by weight eutectic crystal line with a eutectic crystal amount Ec of 10 by weight exists adjacent a high C-concentration side of a solidus, and a 50 by weight eutectic crystal line with a eutectic crystal amount Ec of 50 % by weight 20 exists adjacent a low C- concentration side of a 100 by weight eutectic crystal line with a eutectic crystal amount Ec of 100 % by weight. Three lines between the 10 by weight eutectic crystal line and the 50 % by weight eutectic crystal line are 20, 30 and 40 % by weight eutectic crystal lines in order from 25 the 10 by weight eutectic crystal line, respectively.

For the composition range of the Fe-based alloy material,

the eutectic crystal amount Ec is in a range of 10 by weight < Ec < 50 % by weight and therefore, in a range between the 10 % by weight eutectic crystal line and the 50 % by weight eutectic crystal line. However, compositions on the 10 by weight 5 eutectic crystal line and the 50 % by weight eutectic crystal line are excluded. In addition, the C content is in a range of 1.8 % by weight s C s 2.5 by weight and the Si content is in a range of 1.0 % by weight Si s 3.0 by weight. Hence, when the C content is taken on an X axis, and the Si content 10 is taken on a Y axis in Fig.2, the composition range of the Fe-based alloy material is in a range represented by a substantially hexagonal figure formed by connecting a coordinate (2.08, 1.0) point al, a coordinate (2.5, 1.0) point a2, a coordinate (2.5, 2.6) point a3, a coordinate (2.42, 3.0) 15 point a4, a coordinate (1.8, 3.0) point as end a coordinate (1.8, 2.26) point a6 to one another. However, compositions at the points a3 and a4 lying on the 50 % by weight eutectic crystal line and on a line segment b1 connecting the points a3 and a4, and compositions at the points a1 and a6 lying on the 10 % by 20 weight eutectic crystal line and on a line segment b2 connecting the points a1 and a6 are excluded from the compositions on a profile b of the figure indicating the limit of the composition range. It is desirable that the solid phase rate R of the 25 semi-molten Fe-based alloy material is larger than 50 %. Fig.3

is a graph showing the relationship between a heating temperature and a solid phase rate R for an Fe-C-Sibased alloy.

A line L1 corresponds to the case where the C and Si contents are 1.8 % by weight and 1.0 % by weight which are lower limit 5 values, respectively, and a line L2 corresponds to the case where the C and Si contents are 2.5 by weight and 3.0 by weight which are upper limit values, respectively. It can be seen that if the C and Si contents are smaller than the lower limit values,the casting temperature must tee considerately high 10 in order to provide a solid phase rate R higher than 50 % by weight. Namely,atacastingtemperaturesetfromtheviewpoint of the curability of the pressure casting apparatus end thelike, the solid rate R of the material is high and for this reason, casting defects due to a filling failure or a cold shut are 15 produced. On the other hand,if the C and Si consents are higher than the upper limit values, the solid phase rate R of the materialis lower and for this reason, the chilled structure i, is increased and cracks are liable to be produced.

Table 1 shows the composition and the eutectic crystal 20 amount Ec for example (1) and comparative example (la) of Fe-based alloy material.

Table 1

Chemical constituent Eutectic Fe-based (% by weight) crystal alloy C Si Ni Fe amount Ec material. (% by weight) 2 3 2 o 1.2 1.1 < 0.04 < 0.04 Balance 33 Example (1) _ _ Comparative 2. 3 2.o 0.2 < 0.04 < 0.04 Balance 33 (la) _ Example (1) and comparative example (la) are also shown as points (1) and (la) in Fig.2.

5 To produce a cast product by casting, example (1) was subjected to aninduction heating upto1180 Cwhichis a casting temperature, thereby preparing a semi-molten Fe-based alloy material having solid and liquid phases coexisting therein.

The solid phase rate R of this material was equal to 58 %.

10 Then, the temperature of the stationary and movable dies 2 and 3 in the pressure casting apparatus 1 shown in Fig.1 was controlled, and the semi-molten Fe-based alloy material S was placed into the chamber 6. Thereafter, the pressing plunger 10 was operated to pour the Fe-based alloy material 5 into the 15 cavity 4. In this case, the pouring pressure for the semi molten Fe-based alloy material 5 was 36 MPa. Then, a pressing force was applied to the semi-molten Fe-based alloy material 5 filled in the cavity 4 by retaining the pressing plunger 10 at a terminal end of its stroke, thereby solidifying the 20 semi-molten Fe-based alloy material 5 under such pressure to produce example (1) of a cast product 12 shown in Fig.4. Using

comparative example (la), example (la) of the cast product 12 was produced in a similar manner. However, the casting temperature was set at 1180 C.

In a cavity-correspondence portion 12a of the cast 5 product 12, an area from a site B4 in the vicinity of a gate-correspondence portion 12b and nearer to a tip end of the cavity than the gate-correspondence portion 12b to a base end cofthecavity-corre spondenceportionl2aisascrapSandhence, an area from the site B4 to a tip end e of the cavity 10 correspondence 12a is a product P. Central portions of a tip end portion B1, an intermediate portion B2 and a base end portion B3 in each of the products P of both the cast products 12 were microscopically examined, whereby their cast structures were examined to provide results 15 in Figs.5A to 5C for example (1) of the cast product 12 and in Figs.6A to 6C for example (la) of the cast product 12.

In example (1) of the cast product 12 shown in Figs.5A i to 5C, those areas of the tip end portion B1, the intermediate portion B2 and the base end portion B3,which had been a spherical 20 solid phase, were of a mixed structure of austenite and martensite, and the areas which had been a liquid phase were of a ledeburite structure.

In example (la) of the cast product 12 shown in Figs.6A to 6C, those areas of the tip end portion B1 end theintermediate 25 portion B2 which had been asphericalsolid phase were of a mixed

structure of austenite and martensite; those areas of the base end portion B3 which had been spherical solid phase were of a pearlite structure; and the areas which had been a liquid phase were of a ledeburite structure.

5 In example (1) of the cast product 12 made using example (1), the cast structure of the base end portion B3 was the same as those of the tip end portion B1 and the intermediate portion B2, notwithstanding,that the base end portion B3 was slowly cooled by the heat insulating effect of the scrap S. On the 10 contrary, in example (la) of the cast product 12 made using comparative example (la), the base end portion B3 had a cast structure different from those of the tip end portion B1 and the intermediate portion B2, because the base end portion B3 was slowly cooled by the heat insulating effect of the scrap 15 S and no means for avoiding the slow cooling effect was taken.

A plurality of test pieces including the base end portions B3 were made from examples (1) and (la) of the cast product 12.

Then, the test pieces were subjected to a thermal treatment.

Thereafter, the test pieces were microscopically examined for 20 examination of their thermally-treated structures to provide results shown in Figs.7A, 7B to 9A and 9B.

Figs.7A and7B show thermally treated structures provided by subjecting the test pieces to a ledeburite eliminating thermal treatment for 30 minutes at 900 C and for 60 minutes 25 at 750 C. Fig.7A corresponds to the base end portion B3 of

example (1) of the cast product 12, and Fig.7B corresponds to the base end portion B3 of example (la) of the cast product 12.

Figs.8Aand8B show thermally treated structures provided by subjecting the test pieces to a ledeburite eliminating 5 thermal treatment for 30 minutes at 900 C. Fig.8A corresponds to the base end portion B3 of example (1) of the cast product 12, and Fig.8B corresponds to the base end portion B3 of example (la) of the cast product 12.

Fig.9A and 9B show thermally treated structures provided 10 by subjecting the test pieces to a cementite spheroidizing thermal treatment for 60 minutes at 800 C. Fig.9A corresponds to the base end portion B3 of example (1) of the cast product 12, and Fig.9B corresponds to the base end portion B3 of example (la) of the cast product 12.

15 As is apparent from Figs.7A, 7B to9A and 9B, fine graphite grains having a grain size d equal to or smaller than 10 Am were precipitated in the base end portion B3 of example (1) of the I, cast product i2. This applies to the tip end portion B1 and the intermediate portion B2. As a result, example (1) of the 20 cast product 12 has mechanicalproperties uniform over the whole thereof. On the other hand, coalesced graphite grains having a grain size d larger than 10 Am were precipitated in the base end portion B3 of example (la) of the cast product 12, but each of the tip end portion B1 and the intermediate portion B2 was 25 of a thermally treated structure having fine graphite grains,

as was the base end portion B3 of example (1). As a result, the mechanical properties of the tip end portion Bl and the intermediate portion B2 in example (la) of the cast product 12 are different from those of the base end portion B3.

5 The graphite area rate, the hardness, the Charpy impact value (toughness) and the Young's modulus in the base end portions B3 of examples (1) and (la) of the cast product 12 are as given in Table 2., In this case, the graphite area rate was determined using an image analysis device (1P-1000 PC made by lo Asahi Kasei, Co.) by polishing the test pieces without etching thereof. Table 2

Base end Graphite Young's portion area rate Hardness CharPY mPaC2t modulus of cast (%) HB value (J/cm) (GPa) product Fig.7A 4.3 153 9.0 180 Fig.7B 4.3 162 7.0 180 Fig.8A 4.1 260 7.8 183 Fig.8B 4.1 285 5.5 183 Fig. 9A 3.0 192 8.0 188 Fig.9B 2.5 298 2.1 193 As is apparent from Table 2, the base end portion B3 of 15 example (1) of the cast product 12 shown in each of Figs.7A, 8A and 9A has excellent mechanical properties, as compared with the base end B3 of example (la) of the cast product 12 shown in Figs.7B, 8B and 9B.

r Table 3 shows the composition and the eutectic crystal amount Ec for examples (2) to (4) and comparative examples (2a) to (4a).

Table 3

_. _ __

Fe-based Chemical constituent (% by weight) Eu ectic alloy. _. _ material C Si Mn Ni P S Fe Ec _._. _

I Example (2) 2.3 z.o 0.6 1.1 < 0.04 < 0.04 Balance 33 I Example (3) 1 2 0 2.0 t.z 1.1 < 0.04 < 0.041 Balance 17 l Example (4) 2.0 2.0 < 0.04 Balance I 17 Comparative Example (2a)2.0 2.0 0.6 < 0.04 < 0.04 Balance I 17 Comparative Example (3a)2.0 O.z < 0.04 < 0.04 Balance 17 Comparative 0. 6 3.l < 0.04 < 0.04 Balance 17 Examples (2) to (4) and comparative examples (2a) to (4a) are given as points (2) to (4) and points (2a) to (4a) in Fig.2, respectively. Examples (1) to (4) and comparative examples (la) to (4a) lo of the cast products 12 were produced using the above- described examples (lj to (4) and comparative examples (la) to (4a) in amannersimilartotheabove-describedmanner. Each of example (1) and other examples of the cast product 12 was subjected to an annealing treatment for 30 minutes at 900 C and then 15 microscopically examined for examination of their thermally treated structures.

Table 4 shows results of the above-described experiment.

In Table 4, Ecus in the column of material of die means the

above-described Cu-Be based alloy, and Fe" means an alloy tool steel for a high-temperature die. Further, CON in the column of thermally treated structure means that the grain size of graphite grains is equal to or smaller than 10 m, and "X" means 5 that the grain size of graphite grains is larger than 10 um.

Table 4

Example Casting Material Thermally treated structure of cast temperature of die Tip end Intermediate Base end Scrap product ( C) portion portion portion (1) 1180 Cu O O O O Fe O X (2) 1180 Cu O O O Fe O O O X (3) 1200 Cu O O O O Fe O O O X (4) 1200 Fe O O O X (la) 1180 Cu O O X X (2a) 1220 Fe O X X X (3a) 1220 Fe X X X (4a) 1200 Fe graphite grains were agglomerated at points at crystal grain boundary In Table 4, in examples (1) to (3) of the cast product 12 produced using the stationary and movable dies 2 and 3 made 10 of the Cu-Be based alloy, the thermally treated structures of the products P thereof are uniform, and moreover, the thermally treated structures of the scraps S thereof are equivalent to those of the products P due to the cooling promoting effect of

the stationary and movable dies 2 and 3. However, if the stationary and movable dies 2 and 3 made of the above-described steel, including example (4) of the cast product 12, are used, the cooling promoting effect thereof is inferior to that of the 5 dies made of the Cu-Be based alloy and hence, graphite grains are precipitated in coalesced forms in the scrap S. In examples (la)to (3a) of the cast product 12, an effect of nickel (Ni) is Not obtained, because the Fe-based alloy O materials (la) to(3a)donot containnickel(Ni). As a result, JO in the cases of examples (la) and (2a) of the cast product 12, the thermally treated structures of the products P are non-

uniform over the whore "hereof. In the case of the example (3a) of the cast product12,coalesced graphite grains were dispersed over the whole thereof. In the case of example (4a) of the cast 15 product 12, graphite grains were agglomerated at points at a crystal grain boundary due to the Ni content of the Fe-based alloy material (4a) larger than 3.0 by weight.

i Embodiment II Fig.10 shows a pressure casting apparatus 1 used to 20 produce an oil pump cover by casting. In Fig.10, the same components or portions asthosein the apparatuslshown inFig.1 are designated by the same reference characters as in Fig.1, and the detailed description of them is omitted. A scrap

portion 21 is connected to an oil pump cover 20 shown in Fig.11.

25 In a cavity 4, a scrap portion forming area 4b exists between an oil pump cover forming area 4a and a gate 8. A movable die

2g 3 is provided with a core 22 for forming a central bore 23 in the oil pump cover 20, and a plurality of cores 25 for forming a plurality of bolt bores 24 around the central bore 23. Each of the stationary and movable dies 2 and 3 is formed of a steel 5 such as JIS SKD61 and the like, but may be formed of a copper-based alloy such as a Cu-Be based alloy, a Cu-Cr based alloy, a Cu-Ni based alloy and the like, when it is desired to enhance the cooling,rate.

The relationship between the C and Si contents and the 10 eutectic crystal amount Ec in the Fe-based alloy material is in accordance with Fig.2.

Table 5 shows the composition and the eutectic crystal amount Ec for examples(5) to (13) and comparative examples (5a) to (lea).

: T 0: t cat rat rat Cd of do To Z CO 0 Cal 0 CO o 0 0 o 0 0 0 0 0 _. _ 0 0 0 0 0 0 0 0 0 0 0 0

0,.c to m m m m a: m m m m m m m n m m 0) _ 1 -

0 D r n u \0 n n o o o o o o o o o o o o o o o n 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 o o o o o o o o o o o o o o o U dP ----

Co,] o o o o o0 o o 0 o 0c o 0 0 0 0 0 0 0 0 0 0 0 0 0 0 E o o o o o o o o o o o o o o o 4 _ _ _- _- nl __ __ oc Z _ o - o o o o (D 'CM u E E _ o ' o,,, o _ o o C) a) o uo r o tD 0 o 0 0 o o 0 0 0 0 0 0 0 0 1 : _ _ I _ 1

r o u' r co tD C 1 1 o a o o a a 1 o a, o 1 _ 1 - N i 1 I - 1l r- co 1 C:) t- X) 1 ln a 1 1m 1 N N CM O1 C l 1 _ _ --_ _ _ 1 _1 __ _ - 1

_ _ _ _ _ o - > > > > > 1 _ _ _ _ _ - 1- _ _ _ - 1

- 0 0 0 0 0 0 1 0 0 0 0 0 0 1

E E 1 E X X X E X /1) E E]

In Fig.3, a line L3 indicates the relationship between the heating temperature and the solid phase rate R in example Each of example (5) of the columnar Fe-based alloy 5 material having a diameter of 50 Em and a length of 65 mm and other examples was heated into a semi-molten state to produce the oil pump cover 20 having cored holes 23 and 24 at nine points and having the thinnest portion having a thickness of 2.5 mm using the pressure casting apparatus 1 shown in Fig.10. In this 10 case, the preheating temperature for the dies was set at 2S0 C, and the pressure maintaining time was set at 5 seconds.

Then, the presence or absence of cracks generated in each of the oil pump covers 20 was examined by a red mark check.

Table 6 shows the casting temperature, the solid phase 15 rate R and the presence or absence of cracks for examples (5) to (13) and examples (5a) to (lOa) of the oil pump covers 20.

Examples (5) to (13) and examples (5a) to (lea) correspond to examples (5) to (13) and comparative examples (5a) to (lea) given in Table 5, respectively.

Table 6

Oil pump cover Casting Solid phase rate bus o fr l temperature ( C)1 R (%) l cracks _ _ _ _._ _

(5) 1180 59 absence _ _ _. _

(6) ll9o 60 absence _ _ _,

I (7) 1190 l 55 1 absence I l (8) 1190 60 l absence I I (9) 1 ll9o 60 1 absence I (10) 11200 1 53 absence (11) 1190 66 absence - (12) 1190 1 60 l absence j (13) 11180 1 59 1 absence I (5a) 1190 1 56 I presence | (6a) 1190 | 56 I presence l (7a) 1180 58 | presence (8a) I1180 57 presence I I (9a) 1200 55 1 presence (lOa) 1200 56 l presence | As is apparent from Table 6, no crack was generated in each of examples (5) to (13), whereas cracks were generated in 6 all of examples (5a) to (lea). Fig.12 is a view of the oil pump cover free of cracks, and Fig.13 is a view of the oil pump cover havinglarge fractures and hair cracks generated around the bolt bores. Fig.14 is a view of the oil pump cover having cracks generated by being restrained by the two cores. As compared

with the case where manganese (Mn) is contained alone, the cracks were generated in comparative examples (5a), (6a) and (8a), when the Mn content was equal to or smaller than 0.78 by weight, whereas no crack was generated in examples (5) and 5 (8), because the Mn content was equal to or larger than 0.8 by weight. Therefore, it can be seen that when manganese (Mn) is contained alone, it is necessary to set the Mn content at Mn 0.8 % by weight.

In examples (6), (7), (9) and (11) to (13) in which the lO Mn content was smaller than 0.8 by weight, but Mn 0.6 by weight and Mn + Ni + Tin 0.8 % by weight, no crack was generated, whereas in comparative examples (9a) and (lea) in which Mn + Ni + Ti 0.8 % by weight and yet, the Mn content is smaller than 0,6 by weight, cracks were generated. In this way, it 15 can be seen that when nickel (Ni) and/or titanium (Ti) were contained in addition to manganese (Mn), the Mn content must be equal to or larger than 0.6 % by weight and the Mn+Ni+Ti content must be equal to or larger than 0.8 by weight.

Fig.15 is a photomicrograph of the texture showing the 20 me/allographic structure of example (10) of the oil pump cover.

In Fig.15, a black needle-shaped portion is martensite, a light gray portion adjacent the black needle-shaped portion is austenite. The portion of the mixed structure comprising martensite and austenite is a portion which was a solid phase 25 in the casting. A dark gray portion around the portion which

was the solid phaseisledeburite comprising a eutectic crystal of austenite and cementite, and is a portion which was a liquid phase in the casting.

Fig.16 is a photomicrograph of the texture showing the 5 me/allographic structure ofexample(6a) of the oil pump cover.

In Fig.16, a black portion is a portion which was a solid phase in the above-described casting, and such black portion has a pearlite structure. A dark gray portion around the portion which was the solid phase is ledeburite comprising a eutectic 10 crystal of austenite and cementite, and is a portion which was a liquid phase in the casting. As can be seen from comparison of Figs.15 and 16 with each other, in example (10), austenite exists in the portion which was the solid phase and hence, the entire example (10) includes a large amount of austenite and 15 has an excellent toughness.

Embodiment III An Fe-C (2 by weight) alloy material was selected as the Fe-based alloy material. Fig.17 is an Fe-C based equilibrium diagram, wherein a point A1 of the Fe-C (2 % by 20 weight) alloy material is 740 C.

Fig.18 shows the photomicrographic structure of a material having such composition and produced by a continuous castingprocess,namely, acontinuously-cast material, wherein it can be seen that this me/allographic structure is a mixed 25 structure comprising dendrite and a chilled structure (a white

portion). Fig.l9 shows the photomicrographic structure of a material having such composition and produced by casting using a die, namely, a die-cast material, wherein it can be seen that this me/allographic structure is a structure having a graphite 5 phase precipitated in dendrite.

Then, a columnar Fe-based alloy material 50 having a diameter D of 50 mm and a length L of 65 mm as shown in Fig.20 was fabricated from the continuously-cast material, and thermocouples were embedded into one 5b of end surfaces and an 10 outer peripheral surface 5c of the material 50, respectively.

The position of the thermocouplein the end surface 5a is a point E at a depth of 5 mm from the center O of the end surface, while the position of the thermocouplein the outer peripheralsurface 5b is a point F at a depth of 5 mm from a bisected position in 15 the direction of a generating line. During heating of the material 50r the temperature of the point E is lowest, and this temperature is a criterion in the casting process. Therefore, the point E is defined es a casting reference-temperature point.

The point F is a site which is heated to the highest temperature 20 in the induction heating and hence, the point F is defined as the highesttemperature point.

Fig.21 shows one example of a temperature rise curve provided when the Febased alloy material 50 was subject to an induction heating. In the induction heating, the heating rate 25 is controlled by an on-off control and hence, in the highest-temperature point F intensively influenced by the

turning-on/off, the temperature is lowered slightly at the off-time, but in the casting reference-temperature point E, the temperature is raised substantially rectilinearly, because the point E is less influenced by the turning-on/off. However, the 5 heating rate at the highest- temperature point F is larger than that at the casting reference- temperature point E. Therefore, the average value (HRE + HRF)/2 of the heating rates HRE and HRF at the points E and F is defined as the average heating rate HR, and the maximum temperature gradient TG is 10 defined as being equal to ATmax/d( C/mm) from the maximum value ATmax of the difference AT between the temperatures at the points E and F and the distance d between both the points E and F. The relationship between the average value (HRE + HRF) as well as the maximum temperature gradient TG and the cracking 15 due to the heating of the Fe-based alloy material 50 was examined. The Fe-based alloy material 50 was heated to 740 C (the point Al) at the average heating rate HR set at 2.9 C/sec, 4.7 C/sec, 6. 4 C/sec and 7.2 C/sec. The relationship between 20 the average temperature of the material 50 and the difference AT between the temperatures at the casting reference temperature point P and the highest- temperature point Q was examined, thereby providing a result shown in Fig. 22. The term "average temperature" as used herein means an average value (TE 25 + TF) /2 of temperatures TE and TF at the points E and F. The

maximum temperature gradient TG was calculated from a maximum value of the temperature differences AT and the distance d 34 mm between both the points E and F. The relationship between the maximum temperature gradient TG and the average heating 5 temperature HR was examined, thereby providing a result shown in Fig.23. When the average heating temperature HR was set at 4.7 C/sec in this heating test, cracks were not generated in the Fe-based alloy material, but when the average heating rate HR was set at 6.4 C/sec, cracks were generated in the Fe-based 10 alloy material.

From such results, in the present invention, the average heating rate HR to the point Al is set at HR S 6. 0 C/sec, and the maximum temperature gradient TG oftheinsideof the materiel per unit distance is set at TG 7 C/mm.

15 Then, for comparison, an Fe-based alloy material fabricated from the die-cast material was heated to 740 C (the point Al) at an average heating rate set at 11.74 C/sec, and the relationship between the average temperature of the material and the difference AT between the temperatures at the 20 casting reference-temperature point E and the highest-

temperature point F was examined, thereby providing a result shown in Fig. 24. In this case, the maximum value ATmax of the temperature differences AT was 463.4 C and hence, the maximum temperature gradient TG was 13.6, but cracks were not generated

in the material. This is attributable to the absence of a chilled structure in the material.

B. Ultrasonic velocity measuring test Exampleslto40f test pieces asshowninTable7 were fabricated 5 from the continuously-cast material and the die-cast material made of an Fe-C (2 % by weight) alloy. Each of examples 1 to 4 was of a disk shape having a diameter of 50 mm and a thickness of 30 mm. Examples 1 to 4 were subjected to the ultrasonic velocity measurement. EGTlK made byKusaka Rare Metal Co., was 10 used as an ultrasonic measuring apparatus, and the measurement of the sonic velocity was carried out two times for each of examples 1 to 4 in a state in which a probe of the ultrasonic measuring apparatus was placed against the outer peripheral surface, the center of an end surface and a point of the end 15 surface corresponding to one half of its radius. Results are shown in Table 7.

i,

:; ' Table 7

Sonic velocity Sv (mm/see) Test. Measuring Outer Center One piece Mater1alposition peripheral of end half of surface surface radius Measured 5887 5891 5872 Continuously-cast value 5872 5888 5880 Example 1 material Average 5880 5890 5876 Chilled structure: value presence Total average 5882 value Measured 5861 5869 5862 value 5856 5820 5850 Mold-cast material Example 2 Chilled structure: Average 5859 5845 5856 presence Total average 5853 value Measured 5267 5132 5197 Mold-cast material value 5269 5123 5198 Chilled structure: Example 3 absence Average 5268 5128 5198 value Long flake-formed graphite: presence Total average 5198 value __. Measured 5457 5280 5396 Mold-cast material value 5458 5314 5401 Chilled structure: _ Example 4 absence Average 5458 5297 5399 value Short flake-formed graphite: presence Total average 5384 value Then, each of examples 1 to 4 was subjected to a heating test at various maximum temperature gradients TG, whereby it 5 was observed whether cracks were generated, thereby providing

JO a result shown in Fig.25. The sonic velocities for a spherical graphite cast iron and a steel are also shown in Fig.25. As is apparent from Fig.25, it can be seen that the ultrasonic velocity measurement is an effective means for determining 5 whether the material has a chilled structure, because the sonic velocity for examples 1 and 2 having the chilled structure is remarkably high, as compared with examples 3 and 4 having no chilled structure and an FCD material. It was confirmed that cracks was generated due to the heating at the temperature 10 gradient TG equal to or higher than 7 C/mm in examples 1 and 2 having the sonic velocity Sv equal to or higher than 5,600 m/sec. C. Casting test Example l shown in Table 7 was heated to the point Al at 15 an average heating rate HR equal to 2.9 C/sec and a maximum temperature gradient TG equal to 4.5 C/mm, and example 2 was heated to the point A1 at an average heating rate HR equal to 4.7 C/sec and amaximum temperature gradient TG equalto6. 1 C/mm.

Subsequently, they were heated to about 1,200 C into their 20 semi-molten states. Then, examples 1 and 2 in the semi-molten states were placed into a pressure casting apparatus 1 shown in Fig.1, where they were subjected to a casting process. The resulting cast products were examined and as a result, it was mace clear that they were free of defects such es the coalescence 25 of crystal grains and had a good quality.

' This embodiment is not limited to the Fe-C based alloy material, and is also applicable to the other Fe-based alloy materials such as an Fe-C-Si (1 % by weight) alloy material (point A1: 758 C), an Fe-C-Si (2 % by weight) alloy material 5 (point A1: 780 C), an Fe-C-Si (3 % by weight) alloy material (point A1: 820 C), and the like.

Claims

- 42 72473/001.618

Claims

5 1. A process for heating a thixocast Fe-based alloy material having a chilled structure into a semi-molten state in which solid and liquid phases coexist, the process comprising setting an average rate OR of 5 heating to a point Akin an Fe-C based equilibrium 10 diagram to be in a range of 0.5 C/sec HR < 6 0 C/sec, and setting a maximum temperature gradient TG of the inside of the Fe-based alloy material per unit distance to be at TG < 7 C/mm.

15
2. A process for heating a thixocast Fe-based alloy material according to claim 1, further setting a sonic velocity Sv of said Fe-based alloy material determined by an ultrasonic velocity measurement to be at Sv 5, 600 m/sec.